A hydrogen pump comprises a pump housing and a heating mechanism. The pump housing receives liquid hydrogen through a housing inlet. The heating mechanism vaporizes the liquid hydrogen into gaseous hydrogen. The pump housing releases the gaseous hydrogen through a housing outlet at a predetermined pressure level of the gaseous hydrogen. The pump housing closes the housing outlet such as when the liquid hydrogen in the pump housing falls below a depletion level. The pump housing opens and additional liquid hydrogen enters the pump housing through the housing inlet.
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9. A method of pumping hydrogen, comprising the steps of:
receiving liquid hydrogen in a pump housing from a supply tank;
vaporizing at least a portion of the liquid hydrogen into gaseous hydrogen in the pump housing without the use of a mechanical pump;
releasing the gaseous hydrogen from the pump housing upon attainment of a predetermined pressure; and
venting residual gaseous hydrogen from the pump housing back to the supply tank such that additional liquid hydrogen flows into the pump housing, wherein the venting of residual gaseous hydrogen from the pump housing comprises a step of extracting heat from the residual gaseous hydrogen in a vent line extending through liquid hydrogen contained in an intermediate section located between the supply tank and the pump housing.
16. A passive method of generating gaseous hydrogen from liquid hydrogen, comprising the steps of:
receiving liquid hydrogen in a pump housing from a supply tank through a housing inlet of the pump housing thereof;
closing the housing inlet;
vaporizing at least a portion of the liquid hydrogen into gaseous hydrogen without the use of a mechanical pump;
opening a housing outlet to release the gaseous hydrogen upon attainment of a predetermined pressure within the pump housing;
closing the housing outlet;
opening the housing inlet; and
venting residual gaseous hydrogen from the pump back to the supply tank housing such that additional liquid hydrogen flows into the pump housing, wherein the venting of residual gaseous hydrogen from the pump housing comprises a step of extracting heat from the residual gaseous hydrogen in a vent line extending through liquid hydrogen contained in an intermediate section located between the supply tank and the pump housing.
1. A hydrogen pump, comprising:
a supply tank storing liquid hydrogen;
a pump housing receiving the liquid hydrogen from the supply tank through a housing inlet;
a heating mechanism comprising at least one of a heating element on an exterior of the pump housing and a probe extending into the liquid hydrogen the heating mechanism vaporizing at least a portion of the liquid hydrogen into gaseous hydrogen and increasing a pressure thereof within the pump housing, the pump housing releasing the gaseous hydrogen through a housing outlet upon attainment of a predetermined pressure of the gaseous hydrogen in the pump housing;
the pump housing closing the housing outlet and venting residual gaseous hydrogen from the pump housing to allow additional liquid hydrogen to enter the pump housing through the housing inlet;
a vent line extending between the pump housing and the supply tank; and
a vent valve mounted in the vent line and venting residual gaseous hydrogen from the pump housing to the supply tank to reduce a pressure within the pump housing such that liquid hydrogen flows from the supply tank and into the pump housing;
an intermediate section fluidly connecting the supply tank to the housing inlet and containing liquid hydrogen; and
a heat extraction mechanism comprising a portion of the vent line extending through the liquid hydrogen in the intermediate section and extracting heat from the gaseous hydrogen in the vent line.
4. A passive hydrogen pump, comprising:
a supply tank storing liquid hydrogen;
a pump housing connected to the supply tank and receiving the liquid hydrogen from the supply tank;
an inlet valve interposed between the supply tank and the pump housing;
a heating mechanism comprising at least one of a heating element on an exterior of the pump housing and a probe extending into the liquid hydrogen the heating mechanism vaporizing at least a portion of the liquid hydrogen into gaseous hydrogen within the pump housing and increasing a pressure thereof within the pump housing;
a flow control valve releasing the gaseous hydrogen from the pump housing
upon attainment of a predetermined pressure within the pump housing, the flow control valve closing when the liquid hydrogen in the pump housing falls below a depletion level;
a vent line extending between the pump housing and the supply tank; and a vent valve mounted in the vent line and venting residual gaseous hydrogen from the pump housing to the supply tank to reduce a pressure within the pump housing such that liquid hydrogen flows from the supply tank and into the pump housing;
an intermediate section fluidly connecting the supply tank to a pump housing inlet and containing liquid hydrogen; and
a heat extraction mechanism comprising a portion of the vent line extending through the liquid hydrogen in the intermediate section and extracting heat from the gaseous hydrogen in the vent line.
2. The hydrogen pump of
an inlet valve coupled to the housing inlet and being operative to open such that the liquid hydrogen is received in the pump housing, the inlet valve being operative to close in response to the liquid hydrogen reaching a fill level in the pump housing.
3. The hydrogen pump of
the inlet valve is operative to open in response to the liquid hydrogen falling below a depletion level.
5. The hydrogen pump of
at least one of a fill sensor and a depletion sensor coupled to the pump housing and being configured to sense a fill level of the liquid hydrogen in the pump housing.
6. The hydrogen pump of
when the pressure of the gaseous hydrogen in the pump housing is higher than the pressure of the liquid hydrogen in the intermediate section, the pump housing is configured to open a housing inlet when the liquid hydrogen in the pump housing falls below a depletion level such that gaseous hydrogen in the pump housing flows into the intermediate section and mixes with the liquid hydrogen due to the higher pressure of the gaseous hydrogen in the pump housing relative to the pressure of the liquid hydrogen in the intermediate section.
7. The hydrogen pump of
a diffuser configured to reduce a velocity of gaseous hydrogen discharging from the vent line into the supply tank.
8. The hydrogen pump of
the pump housing includes a horizontal section and a vertical section;
the horizontal section configured for containing the liquid hydrogen; and
the vertical section configured for accumulating the gaseous hydrogen.
10. The method of
sealing the pump housing prior to vaporizing the liquid hydrogen.
11. The method of
heating the liquid hydrogen within the pump housing to increase a pressure of the gaseous hydrogen therewithin.
12. The method of
venting the residual gaseous hydrogen to the supply tank to reduce the pressure within the pump housing such that the additional liquid hydrogen flows into the pump housing.
13. The method of
extracting heat from the residual gaseous hydrogen occurs prior to venting the residual gaseous hydrogen to the supply tank.
14. The method of
15. The method of
increasing a pressure of the gaseous hydrogen in the pump housing higher than the pressure of the liquid hydrogen in the intermediate section; and
opening a housing inlet when the liquid hydrogen in the pump housing falls below a depletion level such that the gaseous hydrogen in the pump housing flows into the intermediate section and mixes with the liquid hydrogen in the intermediate section due to the higher pressure of the gaseous hydrogen in the pump housing relative to the pressure of the liquid hydrogen in the intermediate section.
17. The method of
venting the residual gaseous hydrogen to the supply tank.
18. The method of
extracting heat from the residual gaseous hydrogen prior to venting the residual gaseous hydrogen to the supply tank.
19. The method of
increasing a pressure of the gaseous hydrogen in the pump housing higher than the pressure of the liquid hydrogen in the intermediate section; and
opening the housing inlet when the liquid hydrogen in the pump housing falls below a depletion level such that the gaseous hydrogen in the pump housing flows into the intermediate section and mixes with the liquid hydrogen in the intermediate section due to the higher pressure of the gaseous hydrogen in the pump housing relative to the pressure of the liquid hydrogen in the intermediate section.
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(Not Applicable)
(Not Applicable)
The present invention relates generally to fuel systems and, more particularly, to a system and method for converting liquid hydrogen into gaseous hydrogen.
Hydrogen offers several advantages over petroleum based fuels in terms of reduced emissions and improved fuel efficiency. For example, when hydrogen is used in fuel cells to produce electricity for powering electric motors, the byproduct is water. When hydrogen is burned in an internal combustion engine such as a turbine engine or a piston engine, exhaust gas emissions are relatively low as compared to the emissions resulting from the combustion of petroleum based fuels. Another advantage of hydrogen as a fuel is the generally higher energy-per-mass density as compared to petroleum based fuels such as jet fuel. For example, hydrogen contains approximately three times the energy-per-unit mass of petroleum based fuels.
Hydrogen may be efficiently stored in liquid form in order to minimize the required storage volume. Although storing hydrogen in liquid form requires maintaining the temperature below approximately −420° F., the low pressure at which liquid hydrogen may be stored minimizes the overall weight of the vehicle as compared to the large number of tanks that would be required to store hydrogen in gaseous form.
The above-noted advantages associated with hydrogen may be applied to certain vehicles. For example, high-altitude, long-endurance (HALE) aircraft may benefit from a hydrogen-based propulsion system. HALE aircraft may be designed to operate at altitudes of up to 65,000 feet and may stay aloft for up to fourteen days or longer. However, a variety of other vehicles and systems may benefit from hydrogen as an alternative to petroleum based fuels.
In order to use hydrogen in a fuel cell or in an internal combustion engine, the hydrogen must be in a gaseous state. In addition, it is necessary to increase the pressure of the gaseous hydrogen to suit the operating requirements of the fuel cell or internal combustion engine. Prior art methods for converting liquid hydrogen to gaseous hydrogen at a suitable temperature and pressure include the use of heat exchangers and mechanical pumps. Heat exchangers may be used to vaporize the liquid hydrogen into gaseous hydrogen for use as a fuel. Unfortunately, heat exchangers are typically bulky.
In long endurance applications such as HALE aircraft, mechanical pumps must be capable of operating continuously for extended periods of time. The extremely low temperature of liquid hydrogen and the low viscosity of hydrogen limits the efficiency and reliability of mechanical pumps. More specifically, because of the extremely low temperatures, portions of the mechanical pump that are exposed to the liquid hydrogen may undergo significant thermal contraction. In order to accommodate differences in thermal contraction between various portions of the mechanical pump, the mating components of the pump must be designed and manufactured with relatively large tolerances. However, large tolerances may reduce pump efficiency.
In addition, mechanical pumps typically include rotating components which require lubrication to minimize friction and prevent wear. Unfortunately, the relatively low viscosity of liquid hydrogen minimizes the ability of the hydrogen to act as a lubricant. Furthermore, the low temperature of liquid hydrogen minimizes the available number of compatible lubricants (e.g., Teflon) that may be used in the pump.
As can be seen, there exists a need in the art for a system and method for converting liquid hydrogen into gaseous hydrogen at a suitable operating temperature and pressure. In this regard, there exists a need in the art for a system and method for converting liquid hydrogen into gaseous hydrogen which requires a minimum number of moving parts and wherein gaseous hydrogen may be continuously produced in a reliable and efficient manner.
The above described needs associated with hydrogen fuel are specifically addressed by the present disclosure which provides, in an embodiment, a hydrogen pump comprising a pump housing and a heating mechanism. The pump housing is configured to receive liquid hydrogen through a housing inlet such as from a supply tank. The heating mechanism is configured to vaporize the liquid hydrogen contained within the pump housing to generate gaseous hydrogen.
Furthermore, the heating mechanism is configured to increase the pressure of the gaseous hydrogen such that the gaseous hydrogen may be continuously released from a housing outlet upon attainment of a predetermined pressure of the gaseous hydrogen. The gaseous hydrogen may be continuously released from the housing outlet until the liquid hydrogen in the pump housing falls below a predetermined level at which time the housing outlet may close. Residual gaseous hydrogen may then be vented from the pump housing to facilitate the receiving of additional liquid hydrogen within the pump housing at the start of a new cycle.
In an embodiment, the hydrogen pump may be configured such that the housing inlet opens momentarily (i.e., for a predetermined period of time) after the closing of the housing outlet and prior to venting of the residual gaseous hydrogen. In this manner, the higher pressure gaseous hydrogen within the pump housing flows out of the pump housing through the housing inlet and mixes with liquid hydrogen to reduce the temperature of the gaseous hydrogen.
The hydrogen pump may include an intermediate section interconnecting the pump housing to the supply tank. The intermediate section may contain liquid hydrogen and may provide a location for the mixing of the gaseous hydrogen with the liquid hydrogen. Following the mixing of the gaseous hydrogen with the liquid hydrogen, residual gaseous hydrogen in the pump housing may be vented through a vent line in order to reduce the pressure within the pump housing. The venting of the residual gaseous hydrogen allows the additional liquid hydrogen to flow into the housing inlet at the start of a new cycle. The vent line may optionally be routed through the intermediate section in order to extract the heat of the residual gaseous hydrogen in the vent line prior to delivery of the residual gaseous hydrogen to the supply tank. Extracting the heat from the residual gaseous hydrogen reduces the amount of heat required to vaporize the liquid hydrogen in the pump housing.
The technical benefits of the present disclosure include the combining of vaporization and pumping of hydrogen into a single, passive, closed system without the need for a mechanical pump or a conventional heat exchanger. The passive hydrogen pump provides a means for generating gaseous hydrogen at a desired operating temperature and pressure in an efficient and reliable manner.
The features, functions and advantages that have been discussed can be achieved independently in various embodiments of the present disclosure or may be combined in yet other embodiments, further details of which can be seen with reference to the following description and drawings below.
These and other features of the present disclosure will become apparent upon reference to the drawings wherein like numbers refer to like parts throughout and wherein:
Referring now to the drawings wherein the showings are for purposes of illustrating preferred and various embodiments of the disclosure only and not for purposes of limiting the same, shown in
In a broad sense, the hydrogen pump 10 comprises a pump housing 36 and a heating mechanism 54. The pump housing 36 may be configured for receiving liquid hydrogen 12 through a housing inlet 38. More specifically, the liquid hydrogen 12 may be stored in a supply tank 20 such as a cryogenic supply tank 20 suitable for maintaining the hydrogen at a temperature below approximately −420° F. In this regard, the supply tank 20 may be configured as a cryogenic supply tank 20 employing active and/or passive insulation in order to maintain the hydrogen in a liquid state. However, the supply tank 20 may employ any technique known in the art for maintaining hydrogen in a liquid state. Although shown as a generally spherically shaped container, the supply tank 20 may be provided in any suitable size, shape and configuration, without limitation.
Upon receiving the liquid hydrogen 12 into the pump housing 36, a heating mechanism 54 may be configured to vaporize the liquid hydrogen 12 in the pump housing 36 into gaseous hydrogen 14. In addition, the heating mechanism 54 may be configured to increase the pressure of the gaseous hydrogen 14 in the pump housing 36 to a level that is suitable for use by a component that is downstream of the hydrogen pump 10. For example, for an internal combustion engine, the hydrogen pump 10 may be configured to produce gaseous hydrogen 14 within a temperature range of approximately −10 F.° to 250° F. and within a pressure range of approximately 60 to 100 psia. However, the hydrogen pump 10 may be configured to provide the gaseous hydrogen 14 in any temperature and pressure for use in a wide variety of applications.
Referring still to
Referring briefly to
Advantageously, the hydrogen pump 10 as disclosed herein provides a passive, closed system which combines the requirement of vaporizing liquid hydrogen 12 and continuous pumping of the hydrogen such that gaseous hydrogen 14 may be continuously delivered for downstream use such as in an internal combustion engine, a fuel cell or any other system, environment, application, assembly, structure or vehicle, without limitation. For example, the hydrogen pump 10 may be incorporated into a variety of applications and industries including, but not limited to, refinery operations, food processing, power plant cooling and in nuclear reactor facilities. In addition, the hydrogen pump 10 may be incorporated into a wide variety of manufacturing operations and other processes including, without limitation, heat treating, welding and chemical synthesis.
Referring still to
The vertical section 44 may extend upwardly from the horizontal section 42. As shown in
Although shown in an L-shaped configuration, the pump housing 36 may be provided in any size, shape and configuration which facilitates receiving of the liquid hydrogen 12 and heating thereof. Furthermore, the pump housing 36 may be provided in any configuration which facilitates the vaporization and accumulation of gaseous hydrogen 14 for discharge from the pump housing 36. In this regard, the pump housing 36 may be configured to release the gaseous hydrogen 14 through the housing outlet 40 when the gaseous hydrogen 14 within the pump housing 36 reaches a predetermined pressure. The housing outlet 40 of the pump housing 36 may be configured to close when the liquid hydrogen 12 falls below a predetermined level. In addition, as shown in
The hydrogen pump 10 may include a flow control valve 60 which may be fluidly coupled to or integrated into the housing outlet 40. The flow control valve 60 may include a flow control valve inlet 64 and a flow control valve outlet 66. The flow control valve inlet 64 may be fluidly coupled to the housing outlet 40. The flow control valve outlet 66 may be fluidly coupled to a downstream component via a delivery conduit (not shown) such that the downstream component may receive gaseous hydrogen 14 from the hydrogen pump 10. The flow control valve 60 may be provided in any suitable configuration such as a check valve, a pressure regulator 58 or any other suitable valve arrangement or mechanism which regulates the opening and closing of the housing outlet 40. The flow control valve 60 may include a control valve actuator 62 which may be configured to open the flow control valve 60 to allow for release of the gaseous hydrogen 14 from the pump housing 36 upon attainment of a predetermined pressure of the gaseous hydrogen 14 within the pump housing 36. Furthermore, the flow control valve 60 may be configured to close when the pressure of the gaseous hydrogen 14 falls below a predetermined pressure and/or when the level of the liquid hydrogen 12 in the pump housing 36 falls below a predetermined level such as below a depletion level 53 as illustrated in
In an embodiment, the flow control valve 60 may be regulated in correspondence to a sensed level of the liquid hydrogen 12 within the pump housing 36. For example, the flow control valve 60 or control valve actuator 62 may be communicatively coupled to one or more level sensors which may be mounted within or incorporated into the pump housing 36 such as in the horizontal section 42 as shown in
In an embodiment, the fill sensor 50 may sense when the liquid hydrogen 12 reaches a fill level 51 within the horizontal section 42 of the pump housing 36. The fill sensor 50 may generate signals representative of the attainment of the fill level 51. Such signals may be provided to the flow control valve 60, the inlet valve 30, the vent valve 70 and/or to any other operating mechanism of the hydrogen pump 10. The depletion sensor 52 may be operative to sense and/or indicate when the liquid hydrogen 12 falls below a depletion level 53 which may indicate that the pump housing 36 is empty.
The hydrogen pump 10 may include a sense line 68 which may extend between the flow control valve 60 and the pump housing 36. The sense line 68 may be configured to provide signals representative of a back pressure of the gaseous hydrogen 14 at the housing outlet 40. The back pressure may be sensed by any suitable sensing mechanism such as by one or more pressure transducers (not shown). The buildup of gaseous hydrogen 14 within the pump housing 36 and, more particularly, within the vertical section 44 of the pump housing 36 may be sensed and communicated to the flow control valve 60 via the sense line 68 such that the flow control valve 60 may be regulated accordingly. For example, the flow control valve 60 may open to release the gaseous hydrogen 14 upon attainment of a predetermined pressure within the pump housing 36.
In an embodiment, the flow control valve 60 may be located or positioned at a higher elevation than the pump housing 36 and/or at a higher elevation than the housing outlet 40 to facilitate release of the gaseous hydrogen 14. However, the flow control valve 60 may be located at any elevation relative to the pump housing 36. Likewise, the supply tank 20 may also be positioned at a higher elevation than the housing inlet 38 in order to facilitate gravity feed of the liquid hydrogen 12 to the pump housing 36. However, the schematic illustrations of
Referring still to
Regardless of the specific configuration, the heating mechanism 54 may be configured to increase the temperature of the liquid hydrogen 12. For example, the heating mechanism 54 may be configured to cause gradual vaporization of the liquid hydrogen 12 into gaseous hydrogen 14 or to continuously vaporize the liquid hydrogen 12 into gaseous hydrogen 14. In an embodiment, the heating mechanism 54 may be configured to intermittently or periodically heat the liquid hydrogen 12 to a temperature that causes vaporization. In addition, the heating mechanism 54 may be configured to increase the temperature and/or pressure of the gaseous hydrogen 14 to a level that corresponds to the operating requirements of the downstream component to which the gaseous hydrogen 14 is delivered such as an internal combustion engine.
The hydrogen pump 10 may further include a vent line 74 which may extend from the pump housing 36 to allow venting of gaseous hydrogen 14. In an embodiment shown in
The vent valve 70 may be operative to open in response to receiving a signal indicating that the liquid hydrogen 12 within the pump housing 36 is at or below the depletion level 53. The open vent valve 70 allows the residual gaseous hydrogen 34 to be vented from the pump housing 36 such as to the supply tank 20 as shown in
Referring to
Referring to
In an embodiment of the hydrogen pump 10, the vent line 74 may terminate at the supply tank 20 which may include a diffuser 24 to slow the rate at which the gaseous hydrogen 14 is discharged from the vent line 74. In this regard, the diffuser 24 may prevent or minimize the disturbance of the surface of the liquid hydrogen 12 which may cause splashing within the supply tank 20 and which may cause a pressure drop within the ullage 22 of the supply tank 20 and/or clogging of the diffuser 24. The diffuser 24 may prevent such splashing by preventing direct discharge onto the surface of the liquid hydrogen 12 in the supply tank 20.
The operation of the hydrogen pump 10 will now be described with reference to the flow chart of
As shown in
Referring to
Referring to
As can be seen in
Referring still to
The heating of the liquid hydrogen 12 may be continuous, intermittent and/or on an as-needed basis for generating the gaseous hydrogen 14. In addition, heat may be applied to the liquid hydrogen 12 and/or to the gaseous hydrogen 14 depending upon the requirements of the downstream system to which the gaseous hydrogen 14 may be delivered. In an embodiment, the heating may continue until the liquid hydrogen 12 within the pump housing 36 falls below a predetermined level as may be sensed by the depletion sensor 52 shown in
Referring to
Referring to
Referring still to
Referring to
Referring to
Referring to
Although the hydrogen pump 10 is illustrated and described in an embodiment which may be integrated into the aircraft 100 illustrated in
Additional modifications and improvements of the present disclosure may be apparent to those of ordinary skill in the art. Thus, the particular combination of parts described and illustrated herein is intended to represent only certain embodiments of the present disclosure and is not intended to serve as limitations of alternative embodiments or devices within the spirit and scope of the disclosure.
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Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
May 12 2009 | The Boeing Company | (assignment on the face of the patent) | / | |||
May 12 2009 | WATTS, DANIEL A | The Boeing Company | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 022671 | /0896 |
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